Air/fuel supply system for use in a gas turbine engine
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United States of America Patent
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Jun 17, 2014
Grant Date -
Dec 1, 2011
app pub date -
May 25, 2010
filing date -
May 25, 2010
priority date (Note) -
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status (Latency Note)
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Abstract
A fuel injector for use in a gas turbine engine combustor assembly. The fuel injector includes a main body and a fuel supply structure. The main body has an inlet end and an outlet end and defines a longitudinal axis extending between the outlet and inlet ends. The main body comprises a plurality of air/fuel passages extending therethrough, each air/fuel passage including an inlet that receives air from a source of air and an outlet. The fuel supply structure communicates with and supplies fuel to the air/fuel passages for providing an air/fuel mixture within each air/fuel passage. The air/fuel mixtures exit the main body through respective air/fuel passage outlets.
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